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0 10 -- Q5

Quiz 5

QuestionAnswer
The auxiliary (tail) rotor of a helicopter permits the pilot to compensate for and/or accomplish which of the following - - Only by decreasing the RPM of the main rotor - - Increasing or decreasing the RPM of the main rotor - - It does nothing to compensate. Increasing or decreasing the RPM of the main rotor
The component that transfers the collective and cyclic inputs to the main rotor blades is the: - - Swashplate - - Rotor shaft - - Tail shaft Swashplate
The primary flight controls in a helicopter are; - - Cyclic, collective, and anti-torque pedals. - - Throttle and Rudder Pedal - - Prop Control and mixture controller Cyclic, collective, and anti-torque pedals
The amount of lift produced by a helicopter rotor system is determined by the cyclic pitch of the main rotor system - - False - - True False
Vertical flight of a helicopter is controlled by increasing or decreasing the collective pitch - - True - - False True
The two basic types of powered aircraft are referred to as what? - - Commercial and Private - - Fixed wing and rotor wing. - - Turbine and Prop Fixed wing and rotor wing
What provides the thrust for a Gyrocopter? - - Propeller - - Turbine - - Rotors Propeller
The __________ allows the helicopter main rotor transmission to drive the tail rotor during autorotation. - - Cyclic pitch unit - - Transmision clutch - - Free wheeling unit Free wheeling unit
A helicopter in forward flight, cruise configuration, changes direction by - - Tilting the main rotor disk in the desired direction - - Pushing the main disk forward or aft - - varying the pitch of the main rotor blades Tilting the main rotor disk in the desired direction
Helicopter main rotor blades provide: - - Directional speed - - Lift and Trust - - Braking Lift and Trust
Created by: sampizzuto
 

 



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